Operating Manual

Operator’s Manual M365-491
1-8 Chapter 1
January/2006 General Information
Table 1-2. Specification Compliance
Boeing
D6-36440 DO-160D
Characteristic Section Airbus Section Category
Temperature 7.2.1.1 4.5 A1 modified
Loss of Cooling 7.2.1.2 4.5.4 B
Altitude 7.2.1.3 4.6.1 A1 (15,000 feet)
Decompression 7.2.1.3 4.6.2 A1 (45,100 feet)
Overpressure 7.2.1.3 4.6.3 A1
Touch Temperature 7.2.2 <15°C rise
Temperature Variation 7.2.3 5.0 C
Humidity 7.2.4 6.3.2 A
Waterproofness 7.2.5 10.3.1 W
Vibration (random) 7.2.7 8.7.2 C/C1
Vibration (windmilling) (901164-3) ABD513.5201-01
Curve 4B
Operational Shock 7.2.8 7.2 B (6g)
Magnetic Effect 15.0 C
Crash Safety 7.3 B (20g)
Power Input 7.3.2.1a 16.0 A/E
Power Input, Power Failure 7.3.2.1f >0.85 lagging
Power Input, Input Capacitance
(EMI)
7.3.2.1g <2.5µF/kVA
line-to-line
<0.2µF
line-to-gnd)
Current Harmonics (901164-3) 16.6.2
Voltage Spikes 7.3.2.2 17.0 A
Grounding and Bonding 7.3.2.4
Induced Signal Susceptibility 7.3.3.2 19.0 C
Audio Frequency Conducted
Susceptibility
7.3.3.3 18.3.2 Z modified
Audio Frequency Emissions 7.3.3.5 8.3
Radio Frequency Susceptibility,
Conducted
7.3.3.4.1 20.4 T
Radio Frequency Susceptibility,
Radiated
7.3.3.4.2 20.5 T